Bell 525 Relentless vs Embraer Legacy 650 E vs Leonardo Aw189 vs Piper M600 Sls
The Bell 525 Relentless and Leonardo AW189 are medium/heavy twin‑engine helicopters, while the Embraer Legacy 650E is a large long‑range business jet and the Piper M600 SLS is a single‑engine turboprop. In range, the Legacy 650E is by far the leader, typically offering roughly 3,900–4,000 nautical miles, suited to true intercontinental missions. The Piper M600 SLS is next, generally around 1,300–1,500 nautical miles, aimed at efficient owner‑flown regional trips. The Bell 525 and AW189 have helicopter‑typical ranges that are much shorter than fixed‑wing aircraft, commonly in the several‑hundred‑nautical‑mile class (roughly about 450–550 nm depending on fuel and payload), optimized for point‑to‑point access rather than distance. For passenger capacity, the Legacy 650E typically carries about 10–13 passengers in executive seating. The Bell 525 and AW189 can be configured broadly, often around 12–16 passengers depending on layout and mission. The Piper M600 SLS is the smallest, typically seating one pilot plus up to five passengers.
| Spec | Bell 525 Relentless | AGUSTA / LEONARDO AW189 | Piper M600 SLS |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 1 |
| Total Seats | 18 | 21 | 6 |
| Flight Rules | IFR | IFR | IFR |
| Manufacturer | Bell | Leonardo | Piper |
| Aircraft Name | 525 Relentless | AW189 | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 580 | 651 | 1406 |
| Max Cabin Seats | 16 | 19 | — |
| OEM Verification | VERIFIED | Un-Verified | VERIFIED |
| Useful Load (lbs) | 6675 | — | 2200 |
| Standard Cabin Seats | 16 | 19 | 4 |
| Flight Deck (Base Spec) | Garmin G5000H | EFIS | Garmin G3000 |
| Max Cruise Speed (ktas) | 160 | 155 | 274 |
| Base Aircraft Price (USD) | $15,000,000 | $2,413,000 | $3,081,400 |
| DOC / nm | — | $ 15.57 | $ 2.19 |
| DOC / nm / Seat | — | $ 0.74 | $ 0.55 |
| Direct Operating Cost | — | $ 2,413 | $ 603 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 1 |
| Total Seats | 18 | 21 | 5 |
| Max Cabin Seats | 16 | 19 | — |
| Standard Cabin Seats | 16 | 19 | 4 |
| Lavatory | — | — | No |
| Galley Location | — | — | MID |
| Cabin Pressure (psi) | — | — | 5.6 |
| Galley / Refreshment | — | — | Refreshment Centre |
| SL Cabin Altitude (ft) | — | — | 12600 |
| Max Cabin Altitude (ft) | — | — | 8644 |
| Engine | |||
| FADEC | Dual-Channel | Yes | No |
| Model | CT7-2F1 | CT7-2E1 | PT6A-42A |
| Fuel Type | JetFuel | JetFuel | — |
| TBO (hrs) | 4000 | 4000 | 3600 |
| Horsepower | 1800 | 1983 | 600 |
| No. of Engines | 2 | 2 | 1 |
| Fuel Capacity (gal) | 641 | — | 260 |
| Flat Rating | — | — | ISA + 55 |
| Dimensions | |||
| Width (ft) | 25.77 | — | — |
| Length (ft) | 61.58 | 57.8 | 29.7 |
| Cabin Width (ft) | 7.58 | — | 4.1 |
| Cabin Height (ft) | 4.5 | — | 4 |
| Cabin Length (ft) | 15.5 | — | 12.3 |
| Overall Height (ft) | 18.18 | 16.6 | 11.3 |
| Rotor Diameter (ft) | 54.5 | 48 | — |
| Baggage Volume Ext. (cu. ft) | 128 | 85 | — |
| Cabin Volume (cu. ft) | — | 395 | 165 |
| Wingspan (ft) | — | — | 43.2 |
| Baggage Volume Int. (cu. ft) | — | — | 20 |